EP2216896A2 - Torque oscillation monitoring - Google Patents

Torque oscillation monitoring Download PDF

Info

Publication number
EP2216896A2
EP2216896A2 EP10250046A EP10250046A EP2216896A2 EP 2216896 A2 EP2216896 A2 EP 2216896A2 EP 10250046 A EP10250046 A EP 10250046A EP 10250046 A EP10250046 A EP 10250046A EP 2216896 A2 EP2216896 A2 EP 2216896A2
Authority
EP
European Patent Office
Prior art keywords
torsional oscillation
signal
variations
amplitude
detected
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP10250046A
Other languages
German (de)
French (fr)
Other versions
EP2216896A3 (en
EP2216896B1 (en
Inventor
Albert L. Markunas
Vijay K. Maddali
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hamilton Sundstrand Corp
Original Assignee
Hamilton Sundstrand Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hamilton Sundstrand Corp filed Critical Hamilton Sundstrand Corp
Publication of EP2216896A2 publication Critical patent/EP2216896A2/en
Publication of EP2216896A3 publication Critical patent/EP2216896A3/en
Application granted granted Critical
Publication of EP2216896B1 publication Critical patent/EP2216896B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P23/00Arrangements or methods for the control of AC motors characterised by a control method other than vector control
    • H02P23/04Arrangements or methods for the control of AC motors characterised by a control method other than vector control specially adapted for damping motor oscillations, e.g. for reducing hunting
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P9/00Arrangements for controlling electric generators for the purpose of obtaining a desired output
    • H02P9/10Control effected upon generator excitation circuit to reduce harmful effects of overloads or transients, e.g. sudden application of load, sudden removal of load, sudden change of load

Definitions

  • the invention relates to the detection of torque oscillation in electro-mechanical power generating systems, and more particularly to monitoring torque oscillation in such systems.
  • WFSM wound field synchronous machine
  • An electrical power generation system may alternatively use a regulated permanent magnet machine (PMM) that has a control coil. Current level in the control coil regulates output current of the PMM.
  • PMM permanent magnet machine
  • a control coil current regulator system senses electrical output potential on a DC bus for the electrical power generation system with such a PMM and adjusts the current level in the control level to regulate the DC bus potential.
  • the electrical generator for an electrical power generation system requires a source of mechanical power, typically a prime mover that comprises a gas turbine engine, coupled to it so that it may convert the mechanical power into electrical power.
  • Coupling is by way of a mechanical coupling that comprises at least a driveshaft, and more typically a reduction gearbox and driveshaft combination.
  • a requirement that a single failed generator that causes the shear of a driveshaft not propagate through the gearbox in such a manner as to result in a failure of the driveshaft for the other generator may constrain the mechanical torsional characteristics of the mechanical coupling.
  • the inclusion of relatively soft generator input driveshafts may prevent such shaft shear propagation.
  • the torsional resonant frequencies of the mechanical coupling can occur within the frequency range of an electrical potential regulation system for the electrical power generation system.
  • Such mechanical coupling is subject to various torsional oscillations during operation of the electrical power generation system. During some operating conditions these torsional oscillations may persist, becoming sustained torsional oscillations (STOs). These STOs may lead to fatigue damage of the coupling and may cause catastrophic damage if undetected.
  • STOs sustained torsional oscillations
  • EP-A-2020744 describes an active damping system to detect and suppress STO by means of an STO signal detector that detects an STO signal in the generator output and a feedback loop that introduces a modulation of the generator control current that is out of phase with the detected STO signal to dampen the STO.
  • EP-A-2020744 does not address the function of actually indicating the presence of STO or measuring the torque magnitude of the STO, either as part of such a system to ascertain that the damping action functions properly or as a stand-alone STO monitoring system to measure STO and predict mean-time to failure (MTF) of the mechanical coupling arrangement based on the frequency and magnitude of the STO.
  • MTF mean-time to failure
  • the invention generally comprises a method of detecting and monitoring torsional oscillation in a mechanical coupling between a prime mover and a multiphase alternating current (AC) electrical generator, comprising the steps of: detecting in at least one received signal variations that are indicative of changes in the rotational speed of the electrical generator; extracting information from the detected variations that are indicative of torsional oscillation to produce a torsional oscillation signal that has information relating to at least the amplitude of the torsional oscillation; and monitoring the torsional oscillation signal to determine the presence and severity of the torsional oscillation in the mechanical coupling.
  • AC alternating current
  • Figure 1 is a generalised schematic diagram of a typical electrical generating system that is suitable for incorporating at least one possible embodiment of the invention.
  • Figure 2 is a flow chart for a method of detecting and monitoring torsional oscillation in a mechanical coupling between a prime mover and a multiphase alternating current (AC) electrical generator in the electrical generating system shown in Figure 1 according to at least one possible embodiment of the invention.
  • AC alternating current
  • FIG. 1 is a generalised schematic diagram of a typical electrical generating system 2 that is suitable for incorporating at least one possible embodiment of the invention.
  • the generating system 2 has a prime mover 4 that supplies mechanical power to drive at least one multiphase alternating current (AC) generator 6 by way of a mechanical coupling 8.
  • AC alternating current
  • the prime mover 4 is generally a gas turbine engine
  • the generator 6 is a WFSM or a regulated PMM with a control coil
  • the mechanical coupling 8 is at least a driveshaft, and more commonly a gearbox/driveshaft combination.
  • the generator 6 develops electrical power on a main AC power bus 10.
  • a generator control unit (GCU) 12 monitors the level of electrical potential and current on the power bus 10 by means of an electrical potential sensor 14 that develops a bus potential signal on a bus potential signal line 16 and a bus current sensor 18 that develops a bus current signal on a bus current signal line 20. It also sends a direct current (DC) generator control signal to the generator 6 by way of a generator control signal line 22.
  • DC direct current
  • the generator control signal is a DC exciter current signal. If the generator 6 is a regulated PMM with a control coil, the generator control signal is a DC control coil signal. In either case, the generator 6 may have an integral auxiliary generator 24 comprising an unregulated PMM that provides unregulated multiphase AC output power to the GCU 12 by means of an auxiliary power bus 26.
  • the GCU 12 rectifies the AC power on the auxiliary power bus to DC to develop the generator control signal on the generator control signal line 22.
  • torsional oscillations cause changes in the rotational speed of the generator 6 that occur at the fundamental frequency of the torsional oscillations. It is possible to receive a signal that includes information relating to these variations in rotational speed of the generator 6, preferably within the GCU 12, and alter the generator control signal amplitude at the torsional oscillation fundamental frequency properly phased with respect to the torsional oscillation to dampen or suppress it.
  • EP-A-2020744 does not describe any way of monitoring the level of torsional oscillation, either with or without implementation of such torsional oscillation control or active mechanical damping.
  • Figure 2 is a flow chart for a method of detecting and monitoring torsional oscillation in the mechanical coupling 8 between the prime mover 4 and the generator 6 in the electrical generating system 2 shown in Figure 1 according to at least one possible embodiment of the invention.
  • the first step of the method comprises detecting in at least one received signal variations that are indicative of changes in the rotational speed of the generator 6.
  • the received signal may be a generator position signal from a position sensor (not shown) coupled to the generator 6.
  • it may be at least one phase of the unregulated multiphase AC output power on the auxiliary power bus 26. It may also be the electrical potential signal on the bus potential signal line 16, the electrical current signal on the bus current line 20, or a combination thereof.
  • the second step of the method comprises extracting from the detected variations in the received signal that are indicative of the torsional oscillation information to produce a torsional oscillation signal that has information relating to at least the amplitude of the torsional oscillation. For instance, if the received signal is a generator position signal, the variations in speed indicated by the generator speed signal and the frequency at which these variations occur indicate the angular acceleration of the generator 6. If the received signal is at least one phase of the unregulated multiphase AC output power on the auxiliary power bus 26, the amplitude of the unregulated multiphase AC output power indicates the speed or frequency of the generator 6 and variations in the amplitude and the frequency at which these variations occur indicate angular acceleration of the generator 6.
  • the received signal is the electrical potential signal on the bus potential signal line 16, the electrical current signal on the bus current line 20, or a combination thereof, measuring the zero crossings rate, Luenberger state observation or Kalman filtration thereof indicates the speed or frequency of the generator 6 and variations in the indicated speed and the frequency at which these variations occur indicate angular acceleration of the generator 6. Since torque is the product of the effective moment of inertia and the angular acceleration, the torsional oscillation signal may then simply be the product of a constant and the indicated angular acceleration when the generator 6 is unloaded. An electrical load on the generator 6 increases this value by the torque that the load exerts on the rotor of the generator 6. Therefore, under load, the torsional oscillation signal may be the product of a constant and the indicated angular acceleration added to a variable that represents estimated electrical loading of the generator 6.
  • This extraction step may also include high pass filtering of the torsional oscillation signal to remove any signal content below expected torsional oscillation frequencies that may be due to other factors, such as variations in mechanical energy of the engine 4.
  • This extraction step may also include compensating the amplitude and phase of the torsional oscillation signal for system-induced amplitude and phase shift to more accurately indicate estimated torque in the mechanical coupling 8.
  • the third step of the method comprises monitoring the torsional oscillation signal to determine the presence and severity of torsional oscillations in the mechanical coupling 8.
  • This step may include the steps of monitoring the duration that the torsional oscillation signal amplitude remains above a predetermined threshold amplitude and generating a warning signal when the monitored duration exceeds a predetermined length of time that indicates the presence of potentially dangerous torsional oscillations in the mechanical coupling 8, and optionally initiating a sequence of predetermined steps to alleviate the indicated dangerous level of sustained torsional oscillations that sheds electrical loads to the affected generator 6 or even dropping the affected generator 6 off line.
  • This step may also include the steps of recording the duration of torsional oscillations above several predetermined torque thresholds as indicated by the torsional oscillation signal and comparing the recorded duration to a table of estimated mechanical fatigue as a function of torsional oscillation amplitude and duration to monitor estimated life of the mechanical coupling.
  • This latter step requires the monitoring of the frequency of the torsional oscillation in addition to the amplitude in order to estimate the number of cycles for fatigue life estimation of the mechanical coupling 8.

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Control Of Eletrric Generators (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)

Abstract

A method of detecting and monitoring torsional oscillation in a mechanical coupling between a prime mover and a multiphase alternating current (AC) electrical generator, comprises the steps of: detecting in at least one received signal variations that are indicative of changes in the rotational speed of the electrical generator; extracting information from the detected variations that are indicative of torsional oscillation to produce a torsional oscillation signal that has information relating to at least the amplitude of the torsional oscillation; and monitoring the torsional oscillation signal to determine the presence and severity of the torsional oscillation in the mechanical coupling.

Description

    Field of the Invention
  • The invention relates to the detection of torque oscillation in electro-mechanical power generating systems, and more particularly to monitoring torque oscillation in such systems.
  • Background of the Invention
  • Electrical power generation systems powered by variable speed prime movers that require highly regulated electrical output, such as electrical power generation systems used for aeronautical applications, generally use a wound field synchronous machine (WFSM) that serves as an electrical generator. This is because it is easy to adjust rotor current to regulate electrical output of a WFSM. An electrical power generation system may alternatively use a regulated permanent magnet machine (PMM) that has a control coil. Current level in the control coil regulates output current of the PMM. A control coil current regulator system senses electrical output potential on a DC bus for the electrical power generation system with such a PMM and adjusts the current level in the control level to regulate the DC bus potential.
  • In any case, the electrical generator for an electrical power generation system requires a source of mechanical power, typically a prime mover that comprises a gas turbine engine, coupled to it so that it may convert the mechanical power into electrical power. Coupling is by way of a mechanical coupling that comprises at least a driveshaft, and more typically a reduction gearbox and driveshaft combination. For electrical power generation systems of a dual generator design, a requirement that a single failed generator that causes the shear of a driveshaft not propagate through the gearbox in such a manner as to result in a failure of the driveshaft for the other generator may constrain the mechanical torsional characteristics of the mechanical coupling. The inclusion of relatively soft generator input driveshafts may prevent such shaft shear propagation. However, because of this and other design constraints, the torsional resonant frequencies of the mechanical coupling can occur within the frequency range of an electrical potential regulation system for the electrical power generation system. Such mechanical coupling is subject to various torsional oscillations during operation of the electrical power generation system. During some operating conditions these torsional oscillations may persist, becoming sustained torsional oscillations (STOs). These STOs may lead to fatigue damage of the coupling and may cause catastrophic damage if undetected.
  • EP-A-2020744 describes an active damping system to detect and suppress STO by means of an STO signal detector that detects an STO signal in the generator output and a feedback loop that introduces a modulation of the generator control current that is out of phase with the detected STO signal to dampen the STO.
  • However, EP-A-2020744 does not address the function of actually indicating the presence of STO or measuring the torque magnitude of the STO, either as part of such a system to ascertain that the damping action functions properly or as a stand-alone STO monitoring system to measure STO and predict mean-time to failure (MTF) of the mechanical coupling arrangement based on the frequency and magnitude of the STO.
  • Summary of the Invention
  • The invention generally comprises a method of detecting and monitoring torsional oscillation in a mechanical coupling between a prime mover and a multiphase alternating current (AC) electrical generator, comprising the steps of: detecting in at least one received signal variations that are indicative of changes in the rotational speed of the electrical generator; extracting information from the detected variations that are indicative of torsional oscillation to produce a torsional oscillation signal that has information relating to at least the amplitude of the torsional oscillation; and monitoring the torsional oscillation signal to determine the presence and severity of the torsional oscillation in the mechanical coupling.
  • Description of the Drawings
  • Figure 1 is a generalised schematic diagram of a typical electrical generating system that is suitable for incorporating at least one possible embodiment of the invention.
  • Figure 2 is a flow chart for a method of detecting and monitoring torsional oscillation in a mechanical coupling between a prime mover and a multiphase alternating current (AC) electrical generator in the electrical generating system shown in Figure 1 according to at least one possible embodiment of the invention.
  • Detailed Description
  • Figure 1 is a generalised schematic diagram of a typical electrical generating system 2 that is suitable for incorporating at least one possible embodiment of the invention. The generating system 2 has a prime mover 4 that supplies mechanical power to drive at least one multiphase alternating current (AC) generator 6 by way of a mechanical coupling 8. For example, in aeronautical applications, the prime mover 4 is generally a gas turbine engine, the generator 6 is a WFSM or a regulated PMM with a control coil and the mechanical coupling 8 is at least a driveshaft, and more commonly a gearbox/driveshaft combination.
  • The generator 6 develops electrical power on a main AC power bus 10. A generator control unit (GCU) 12 monitors the level of electrical potential and current on the power bus 10 by means of an electrical potential sensor 14 that develops a bus potential signal on a bus potential signal line 16 and a bus current sensor 18 that develops a bus current signal on a bus current signal line 20. It also sends a direct current (DC) generator control signal to the generator 6 by way of a generator control signal line 22. As the GCU 12 monitors the level of electrical potential and current on the power bus 10, it may change the level of the generator control signal on the generator control signal line 22 to maintain a constant predetermined level of electrical potential on the power bus 10.
  • If the generator 6 is a WFSM, the generator control signal is a DC exciter current signal. If the generator 6 is a regulated PMM with a control coil, the generator control signal is a DC control coil signal. In either case, the generator 6 may have an integral auxiliary generator 24 comprising an unregulated PMM that provides unregulated multiphase AC output power to the GCU 12 by means of an auxiliary power bus 26. The GCU 12 rectifies the AC power on the auxiliary power bus to DC to develop the generator control signal on the generator control signal line 22.
  • As described in EP-A-2020744 , torsional oscillations cause changes in the rotational speed of the generator 6 that occur at the fundamental frequency of the torsional oscillations. It is possible to receive a signal that includes information relating to these variations in rotational speed of the generator 6, preferably within the GCU 12, and alter the generator control signal amplitude at the torsional oscillation fundamental frequency properly phased with respect to the torsional oscillation to dampen or suppress it. However, EP-A-2020744 does not describe any way of monitoring the level of torsional oscillation, either with or without implementation of such torsional oscillation control or active mechanical damping.
  • Figure 2 is a flow chart for a method of detecting and monitoring torsional oscillation in the mechanical coupling 8 between the prime mover 4 and the generator 6 in the electrical generating system 2 shown in Figure 1 according to at least one possible embodiment of the invention. The first step of the method comprises detecting in at least one received signal variations that are indicative of changes in the rotational speed of the generator 6. For instance, the received signal may be a generator position signal from a position sensor (not shown) coupled to the generator 6. Alternatively, it may be at least one phase of the unregulated multiphase AC output power on the auxiliary power bus 26. It may also be the electrical potential signal on the bus potential signal line 16, the electrical current signal on the bus current line 20, or a combination thereof.
  • The second step of the method comprises extracting from the detected variations in the received signal that are indicative of the torsional oscillation information to produce a torsional oscillation signal that has information relating to at least the amplitude of the torsional oscillation. For instance, if the received signal is a generator position signal, the variations in speed indicated by the generator speed signal and the frequency at which these variations occur indicate the angular acceleration of the generator 6. If the received signal is at least one phase of the unregulated multiphase AC output power on the auxiliary power bus 26, the amplitude of the unregulated multiphase AC output power indicates the speed or frequency of the generator 6 and variations in the amplitude and the frequency at which these variations occur indicate angular acceleration of the generator 6. If the received signal is the electrical potential signal on the bus potential signal line 16, the electrical current signal on the bus current line 20, or a combination thereof, measuring the zero crossings rate, Luenberger state observation or Kalman filtration thereof indicates the speed or frequency of the generator 6 and variations in the indicated speed and the frequency at which these variations occur indicate angular acceleration of the generator 6. Since torque is the product of the effective moment of inertia and the angular acceleration, the torsional oscillation signal may then simply be the product of a constant and the indicated angular acceleration when the generator 6 is unloaded. An electrical load on the generator 6 increases this value by the torque that the load exerts on the rotor of the generator 6. Therefore, under load, the torsional oscillation signal may be the product of a constant and the indicated angular acceleration added to a variable that represents estimated electrical loading of the generator 6.
  • This extraction step may also include high pass filtering of the torsional oscillation signal to remove any signal content below expected torsional oscillation frequencies that may be due to other factors, such as variations in mechanical energy of the engine 4. This extraction step may also include compensating the amplitude and phase of the torsional oscillation signal for system-induced amplitude and phase shift to more accurately indicate estimated torque in the mechanical coupling 8.
  • The third step of the method comprises monitoring the torsional oscillation signal to determine the presence and severity of torsional oscillations in the mechanical coupling 8. This step may include the steps of monitoring the duration that the torsional oscillation signal amplitude remains above a predetermined threshold amplitude and generating a warning signal when the monitored duration exceeds a predetermined length of time that indicates the presence of potentially dangerous torsional oscillations in the mechanical coupling 8, and optionally initiating a sequence of predetermined steps to alleviate the indicated dangerous level of sustained torsional oscillations that sheds electrical loads to the affected generator 6 or even dropping the affected generator 6 off line. This step may also include the steps of recording the duration of torsional oscillations above several predetermined torque thresholds as indicated by the torsional oscillation signal and comparing the recorded duration to a table of estimated mechanical fatigue as a function of torsional oscillation amplitude and duration to monitor estimated life of the mechanical coupling. This latter step requires the monitoring of the frequency of the torsional oscillation in addition to the amplitude in order to estimate the number of cycles for fatigue life estimation of the mechanical coupling 8.
  • The described embodiments of the invention are only some illustrative implementations of the invention wherein changes and substitutions of the various parts and arrangement thereof may be within the scope of the invention which is set forth in the attached claims.

Claims (14)

  1. A method of detecting and monitoring torsional oscillation in a mechanical coupling (8) between a prime mover (4) and a multiphase alternating current (AC) electrical generator (6), comprising the steps of:
    detecting in at least one received signal variations that are indicative of changes in the rotational speed of the electrical generator;
    extracting information from the detected variations that are indicative of torsional oscillation to produce a torsional oscillation signal that has information relating to at least the amplitude of the torsional oscillation; and
    monitoring the torsional oscillation signal to determine the presence and severity of the torsional oscillation in the mechanical coupling.
  2. The method of Claim 1, wherein the step of detecting variations in at least one received signal comprises detecting variations in a received generator position signal.
  3. The method of Claim 1, wherein the step of detecting variations in at least one received signal comprises detecting variations in a received generator output signal.
  4. The method of Claim 3, wherein the received generator output signal is an unregulated auxiliary permanent magnet machine (PMM) signal.
  5. The method of Claim 4, wherein the step of extracting information from the detected variations in the received signal comprises detecting the amplitude of the unregulated auxiliary PMM signal.
  6. The method of Claim 3, wherein the step of detecting variations in at least one received signal comprises detecting zero crossings of at least one phase of the electrical generator output and the step of extracting information from the detected variations in the received signal comprises the step of measuring the zero crossings rate to produce the torsional oscillation signal.
  7. The method of Claim 3, wherein the step of detecting variations in at least one received signal comprises detecting electrical potential and current levels in at least one phase of the electrical generator output.
  8. The method of Claim 7, wherein the step of extracting information from the detected variations in the received signal comprises the step of analysing the detected electrical potential and current levels in at least one phase of the electrical generator output to produce the torsional oscillation signal.
  9. The method of Claim 8, wherein the step of extracting information from the detected variations in the received signal comprises the step of analysing the detected electrical potential and current levels in at least one phase of the electrical generator output by way of Luenberger state observation to produce the torsional oscillation signal.
  10. The method of Claim 8, wherein the step of extracting information from the detected variations in the received signal comprises the step of analysing the detected electrical potential and current levels in at least one phase of the electrical generator output by way of Kalman filtration to produce the torsional oscillation signal.
  11. The method of any preceding Claim, wherein the step of extracting information from the detected variations in the received signal torsional oscillation to produce a torsional oscillation signal that has information relating to at least the amplitude of the torsional oscillation comprises the step of high pass filtering the torsional oscillation signal to remove any signal content below expected torsional oscillation frequencies.
  12. The method of any preceding Claim, wherein the step of extracting information from the detected variations in the received signal indicative of torsional oscillation to produce a torsional oscillation signal that has information relating to at least the amplitude of the torsional oscillation comprises the step of compensating the amplitude and phase of the torsional oscillation signal for amplitude and phase shift to more accurately indicate estimated torque in the mechanical coupling.
  13. The method of any preceding Claim, wherein the step of monitoring the torsional oscillation signal to determine the presence and severity of torsional oscillation comprises the steps of monitoring the duration that the torsional oscillation signal amplitude remains above a predetermined threshold amplitude and generating a warning signal when the monitored duration exceeds a predetermined length of time that indicated the presence of potentially dangerous torsional oscillations in the mechanical coupling.
  14. The method of any preceding Claim, wherein the step of extracting information from the detected variations that are indicative of torsional oscillation to produce a torsional oscillation signal that has information relating to at least the amplitude of the torsional oscillation extracts angular acceleration of the generator from detected variations in the indicated speed and the frequency at which these variations occur to produce the torsional oscillation signal.
EP10250046.9A 2009-01-12 2010-01-12 Torque oscillation monitoring Active EP2216896B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/352,050 US8056417B2 (en) 2009-01-12 2009-01-12 Torque oscillation monitoring

Publications (3)

Publication Number Publication Date
EP2216896A2 true EP2216896A2 (en) 2010-08-11
EP2216896A3 EP2216896A3 (en) 2014-02-26
EP2216896B1 EP2216896B1 (en) 2018-04-04

Family

ID=42286661

Family Applications (1)

Application Number Title Priority Date Filing Date
EP10250046.9A Active EP2216896B1 (en) 2009-01-12 2010-01-12 Torque oscillation monitoring

Country Status (2)

Country Link
US (1) US8056417B2 (en)
EP (1) EP2216896B1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014209542A1 (en) * 2013-06-25 2014-12-31 Siemens Energy, Inc. Using static excitation system to reduce the amplitude of torsional oscillations due to fluctuating industrial loads
EP2843827A1 (en) * 2013-08-02 2015-03-04 Hamilton Sundstrand Corporation Systems and methods for controlling torsional oscillation in wound field synchronous generator machines
EP3396848A1 (en) * 2017-04-28 2018-10-31 The Boeing Company Systems and methods for reducing effects of torsional oscillation for electrical power generation

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2625498A1 (en) * 2010-10-08 2013-08-14 Rolls-Royce Corporation System and method for detecting fault conditions in a drivetrain using torque oscillation data
US9285386B2 (en) 2013-12-06 2016-03-15 Rosemount Aerospace Inc. Inductive rotational speed sensors
EP3194924B1 (en) * 2014-09-05 2019-11-27 ABB Schweiz AG Monitoring torsional oscillations in a turbine-generator
US11279240B2 (en) 2019-07-16 2022-03-22 Ford Global Technologies, Llc Torque vectoring with model-predictive torque requests

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2020744A2 (en) 2007-07-02 2009-02-04 Hamilton Sundstrand Corporation Active damping for synchronous generator torsional oscillations

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2655036A (en) * 1947-10-01 1953-10-13 Gen Motors Corp Frequency modulated torsional vibration analyzer
US4080559A (en) * 1976-11-15 1978-03-21 General Electric Company Torsional protective device for power system stabilizer
US7832289B2 (en) * 2007-01-06 2010-11-16 Garshelis Ivan J Devices and methods for detecting rates of change of torque
CN100553067C (en) * 2008-01-17 2009-10-21 四方电气(集团)有限公司 The coordination method of shafting torsional vibration of turbo-generator set protection
DE102008025944C5 (en) * 2008-05-30 2013-08-22 Repower Systems Se Monitoring device for pitch systems of wind turbines

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2020744A2 (en) 2007-07-02 2009-02-04 Hamilton Sundstrand Corporation Active damping for synchronous generator torsional oscillations

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014209542A1 (en) * 2013-06-25 2014-12-31 Siemens Energy, Inc. Using static excitation system to reduce the amplitude of torsional oscillations due to fluctuating industrial loads
CN105393449A (en) * 2013-06-25 2016-03-09 西门子能源公司 Using static excitation system to reduce the amplitude of torsional oscillations due to fluctuating industrial loads
US9899942B2 (en) 2013-06-25 2018-02-20 Siemens Energy, Inc. Using static excitation system to reduce the amplitude of torsional oscillations due to fluctuating industrial loads
EP2843827A1 (en) * 2013-08-02 2015-03-04 Hamilton Sundstrand Corporation Systems and methods for controlling torsional oscillation in wound field synchronous generator machines
US9143070B2 (en) 2013-08-02 2015-09-22 Hamilton Sundstrand Corporation Systems and methods for controlling torsional oscillation in wound field synchronous generator machines
EP3396848A1 (en) * 2017-04-28 2018-10-31 The Boeing Company Systems and methods for reducing effects of torsional oscillation for electrical power generation
US10320314B2 (en) 2017-04-28 2019-06-11 The Boeing Company Systems and methods for reducing effects of torsional oscillation for electrical power generation

Also Published As

Publication number Publication date
US8056417B2 (en) 2011-11-15
EP2216896A3 (en) 2014-02-26
US20100175478A1 (en) 2010-07-15
EP2216896B1 (en) 2018-04-04

Similar Documents

Publication Publication Date Title
EP2216896B1 (en) Torque oscillation monitoring
US7808215B2 (en) Active damping for synchronous generator torsional oscillations
EP2118996B1 (en) Load angle measurement and pole slip detection
RU2470182C2 (en) Method of windmill operation control at surges in electric circuit
EP3048333A1 (en) Method and system for damping torsional oscillations
US20060232250A1 (en) Integrated torsional mode damping system and method
US11515764B2 (en) Method and a device for determination of a torsional deflection of a rotation shaft and of a DC-link degradation in the electromechanical drivetrain
CN113228442A (en) Method for determining the location of a short-circuit fault in a generator arrangement, wind turbine, computer program and electrically readable medium
JP2009133810A (en) Vibration monitoring device
JP2024026362A (en) Control device, motor compressor, detection method of ripple voltage and program
JP2011055583A (en) Resonance reduction method and resonance reduction device
EP3194924B1 (en) Monitoring torsional oscillations in a turbine-generator
WO2017103233A1 (en) Multi-stage synchronous generator
JP5051528B2 (en) Machine equipment abnormality judgment device and machine equipment abnormality judgment method
Tsypkin Vibration of induction motors operating with variable frequency drives—A practical experience
US10992162B2 (en) Method for detecting a state of a vehicle electric system
Sihler et al. Torsional Mode Damping For Electrically Driven Gas Compression Trains In Extended Variable Speed Operation.
US10393196B2 (en) Engine accessory disconnect system
EP2061148A1 (en) Protection of variable frequency power systems from excessive peak electrical potentials
Finley et al. Motor vibration problems—Understanding and identifying
JP6783498B2 (en) Shaft torsion vibration suppression control device
EP4177623A1 (en) Generator failure detection method
Luo et al. Keyphasor® based torsional vibration detection and field applications
EP3485242B1 (en) Apparatus and method for the management of an industrial plant comprising electrical machines interacting with energy converters
WO2018089228A1 (en) Bearing fault detection system for an alternator

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR

AX Request for extension of the european patent

Extension state: AL BA RS

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR

AX Request for extension of the european patent

Extension state: AL BA RS

RIC1 Information provided on ipc code assigned before grant

Ipc: H02P 9/10 20060101ALI20140120BHEP

Ipc: H02P 23/04 20060101AFI20140120BHEP

17P Request for examination filed

Effective date: 20140826

RBV Designated contracting states (corrected)

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20171016

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 986622

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180415

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602010049624

Country of ref document: DE

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20180404

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180704

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180704

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180705

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 986622

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180404

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180806

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602010049624

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

26N No opposition filed

Effective date: 20190107

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190112

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20190131

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190131

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190112

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190112

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180804

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20100112

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180404

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230522

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20231219

Year of fee payment: 15

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20231219

Year of fee payment: 15

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20231219

Year of fee payment: 15